Author: Joseph F. Wasserbauer
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32
Book Description
Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Author: Joseph F. Wasserbauer
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32
Book Description
Performance of Small (100-lb Thrust) Rocket Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
Author: Joseph F. Wasserbauer
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
An investigation was conducted on a small (approximately 100-lb thrust) rocket using coaxial injection of N2H4 and N204. Characteristicvelocity efficiencies of 94% of the theoretical shifting equilibrium value were obtained at a chamber pressure of about 300 psi using a 21tube injector and a combustion chamber characteristic length of 10 inches. Performance at lower chamber pressures could be improved by reducing contraction ratio and thereby increasing the combustion chamber length and injector pressure drop, which would tend to promote better mixing. Calculations based on experimental data showed a vacuum specific impulse of 305 sec. with a nozzle area ratio of 50. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
An investigation was conducted on a small (approximately 100-lb thrust) rocket using coaxial injection of N2H4 and N204. Characteristicvelocity efficiencies of 94% of the theoretical shifting equilibrium value were obtained at a chamber pressure of about 300 psi using a 21tube injector and a combustion chamber characteristic length of 10 inches. Performance at lower chamber pressures could be improved by reducing contraction ratio and thereby increasing the combustion chamber length and injector pressure drop, which would tend to promote better mixing. Calculations based on experimental data showed a vacuum specific impulse of 305 sec. with a nozzle area ratio of 50. (Author).
Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide
NASA Technical Note
Comparison of Hydrazine Nitrogen Tetroxide and Hydrazine Chlorine Trifluoride in Small Scale Rocket Chambers
Author: R. James Rollbuhler
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Fuel
Languages : en
Pages : 20
Book Description
Applied Mechanics Reviews
U.S. Government Research Reports
Handling Hazardous Materials
Author: D. R. Cloyd
Publisher:
ISBN:
Category : Chemicals
Languages : en
Pages : 106
Book Description
Publisher:
ISBN:
Category : Chemicals
Languages : en
Pages : 106
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
Book Description